View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 66988U 26145.15497815 +.00000000 +00000-0 +21450-3 0 00003
2 66988 97.5027 215.4753 0003500 118.2553 241.9037 15.23689916 05
| Epoch (UTC): | 25 May 2026 03:43:10 |
| Eccentricity: | 0.0003500 |
| inclination: | 97.5027° |
| perigee height: | 492 km |
| apogee height: | 497 km |
| right ascension of ascending node: | 215.4753° |
| argument of perigee: | 118.2553° |
| revolutions per day: | 15.23689916 |
| mean anomaly at epoch: | 241.9037° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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